For the case when the reflected signal does not differ from the true one by more than 8.5–10 dB, the dynamic range of the level changes in the SRNS, which depends on the difference between the conditions in the transmission of navigation signals from SC, which form the working constellation, is approximately the same.
Improvement of Noise Immunity of Navigation Systems of Aircraft of Civil Aviation on the Basis of Satellite and Inertial Navigation System and Also Ground-Based Systems
Springer Aerospace Techn.
Modern Requirements for Noise Immunity Aircraft Navigation Equipment ; Chapter : 4 ; 149-171
2021-05-14
23 pages
Article/Chapter (Book)
Electronic Resource
English
Satellite Navigation in Civil Aviation
NTIS | 1988
|Combined inertial - ILS aircraft navigation systems
AIAA | 1971
|